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Referencia: 92/91
Brida rodamientos autolubricantes 6 x 10 x 3 mm
Política de seguridad
Política de envío
Política de devolución
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Riferimento: 214/16
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
Riferimento: 268/16
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
Riferimento: 340/16
This exhaust system is designed for the Lama with turbine power system.
Riferimento: 791/16
Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards the rear.
Riferimento: 350/17
When the turbine of a full-size helicopter is not running, the engine is protected with an exhaust cover which prevents foreign objects finding their way inside the turbine. This exhaust cover for model turbines is suitable for the Lama, Alouette III and any other machine with a 90 mm Ø exhaust pipe. Caution: it is essential to allow the exhaust pipes to...
Riferimento: 206/16
This exhaust system is designed for the UH-1D with turbine power system.Exhaust tubes for turbines are always designed for the specified model. It is important that no forward thrust emerges from the system. Should this still occur, the forward thrust produced is minimal.Turbine exhaust tubes are designed as exhaust-gas diffusers, i.e. opens wider towards...
Riferimento: 770/16
On the BK 117 the forward thrust is eliminated by the scale division of the exhaust tube (enlarging of the cross-section) and exhausting up through the rotor disc.
Riferimento: 930/16
right / leftThis exhaust system is designed for the Mil Mi-2 with turbine power system.
